Ex Parte Slowik et alDownload PDFPatent Trial and Appeal BoardDec 17, 201813926733 (P.T.A.B. Dec. 17, 2018) Copy Citation UNITED STA TES p A TENT AND TRADEMARK OFFICE APPLICATION NO. FILING DATE FIRST NAMED INVENTOR 13/926,733 06/25/2013 138462 7590 12/19/2018 ANSALDO/STUDIO TORTA c/o BUCHANAN INGERSOLL & ROONEY PC P.O. BOX 1404 ALEXANDRIA, VA 22313 Slawomir Slowik UNITED STATES DEPARTMENT OF COMMERCE United States Patent and Trademark Office Address: COMMISSIONER FOR PATENTS P.O. Box 1450 Alexandria, Virginia 22313-1450 www .uspto.gov ATTORNEY DOCKET NO. CONFIRMATION NO. 0087748-000069 5596 EXAMINER DUNLAP, JONATHAN M ART UNIT PAPER NUMBER 2855 NOTIFICATION DATE DELIVERY MODE 12/19/2018 ELECTRONIC Please find below and/or attached an Office communication concerning this application or proceeding. The time period for reply, if any, is set in the attached communication. Notice of the Office communication was sent electronically on above-indicated "Notification Date" to the following e-mail address(es): ADIPDOCl@BIPC.COM PTOL-90A (Rev. 04/07) UNITED STATES PATENT AND TRADEMARK OFFICE BEFORE THE PATENT TRIAL AND APPEAL BOARD Ex parte SLA WO MIR SLOWIK, THOMAS TSCHARNER, PIOTR BEDNARZ, and MICHAL TOMASZ PRUGAREWICZ Appeal2018-002309 Application 13/926,733 Technology Center 2800 Before MICHELLE N. ANKENBRAND, A VEL YN M. ROSS, and MERRELL C. CASHION, JR., Administrative Patent Judges. CASHION, Administrative Patent Judge. DECISION ON APPEAL STATEMENT OF THE CASE This is an appeal under 35 U.S.C. § 134(a) from a final rejection of claims 1, 3-9, 12-16, and 18-23. 1 We have jurisdiction under 35 U.S.C. § 6. We AFFIRM. 1 Although the Examiner did not list claim 9 in the "Disposition of Claims" section of the Final Office Action, the Examiner did reject claim 9 in the Final Office Action and both the Examiner and Appellant acknowledges that claim 9 is part of this appeal. Ans. 2; App. Br. 7. Appeal2018-002309 Application 13/926,733 The invention is directed to a method to determine the appropriate time to replace a rotor by determining the extent of creeping (time dependent plastic expansion) in the rotor as a result of exposure to high temperature operating conditions. Spec. ,r 3. This is done through the use of marks distributed along the rotor's surface to allow for separate measurements along the geometry of the rotor at different points in time, such as when it is first placed in service and after operation, to determine the amount of creeping from the comparison of these measurements. Id. ,r 14. Claim 1 is illustrative of the subject matter on appeal and is reproduced below: 1. A method for measuring geometry deformations of a rotor having a rotor groove with a fir-tree configuration, the method comprising: engraving the rotor groove in various locations with measuring marks; using the measuring marks as a reference point in determining, in a first measurement, a length on said rotor groove prior to the turbine being placed into service; operating the turbine for a period of time; determining, in a second measurement, the length on said rotor groove using again the measuring marks as a reference point, after the operating period; comparing the measured lengths of said first and second measurements; and determining an amount of creep deformation in said rotor groove based on a difference between the measured lengths. App. Br. Claims App'x 1. 2 Appeal2018-002309 Application 13/926,733 Appellant2 (see generally App. Br.) requests review of the following rejections from the Examiner's Final Action: I. Claims 1, 3-8, 12-16, and 18-23 rejected under pre-AIA 35 U.S.C. § I03(a) as unpatentable over Telfer (US 8,818,078 B2, issued August 26, 2014), Pross (US 2002/0019708 Al, published February 14, 2002) and Hovel (US 2011/0099809 Al, published May 5, 2011). II. Claim 9 rejected under pre-AIA 35 U.S.C. § I03(a) as unpatentable over Telfer, Pross, Hovel, and Kamegawa (US 5,568,259, issued October 22, 1996). Appellant relies on the same line of arguments in addressing independent claims 1, 13, and 21. See generally App. Br. Appellant does not present separate arguments for the dependent claims subject to either Rejection I or II. Accordingly, we select claim 1 as representative of the subject matter for review on appeal for this rejection. Claims 3-9, 12-16, and 18-23 stand or fall with claim 1. OPINION After review of the respective positions provided by Appellant and the Examiner, we AFFIRM the Examiner's prior art rejections of claims 1, 3-9, 12-16, and 18-23 for the reasons presented by the Examiner. We add the following for emphasis. With respect to claim 1, the Examiner finds that the combined teachings of Telfer and Pross disclose a method for measuring geometry deformations of a rotor that differs from the claimed invention in that Telfer and Pross do not teach engraving the markings on a rotor. Final Act. 2--4. The Examiner finds Hovel discloses laser engraving markings on a turbine 2 ALSTOM Technology Ltd.is the Applicant/ Appellant. Ansaldo Energia IP UK Limited is identified as the real party in interest. App. Br. 2. 3 Appeal2018-002309 Application 13/926,733 component to provide an accurate and permanent marking for a visual coordinate system used for repairing a damaged turbine component. Final Act. 4; Hovel ,r,r 15, 46. The Examiner determines it would have been obvious to one of ordinary skill in the art to utilize engraved markings in Telfer's method, as modified by Pross, to provide a permanent marking as an accurate reference point for optical measurements of turbine components (e.g., rotors). Final Act. 4; Hovel ,r,r 46-47. Appellant argues none of the cited references discloses or suggests engraving measuring marks in various locations of a surface of a rotor groove, comparing the measured lengths of the first and second measurements, and determining an amount of creep deformation in the rotor groove based on a difference between the measured lengths. Id. at 4. Specifically, Appellant argues that Pross discloses monitoring at least one test element, which is exposed to an operating load comparable to that of the component to be monitored. Id. at 5-6. Thus, Appellant contends that Pross does not disclose engraving a rotor as claimed. Id. at 6. We are unpersuaded by these arguments. It is well-established that nonobviousness cannot be established by attacking the references individually when the rejection is predicated upon a combination of prior art disclosures. In re Merck & Co., 800 F.2d 1091, 1097 (Fed. Cir. 1986); In re Keller, 642 F.2d 413, 425-26 (CCPA 1981) ("The test [for obviousness] is what the combined teachings of the references would have suggested to those of ordinary skill in the art."). Appellant's arguments are unavailing because they do not address the rejection the Examiner presented. As the Examiner finds, Pross discloses that it was known to monitor creep in a rotor of a gas turbine engine. Ans. 4; 4 Appeal2018-002309 Application 13/926,733 Pross ,r,r 1-2. Appellant's Specification also acknowledges this fact. Spec. ,r 5 and Figure 1 ( describing what was known in the art as to measuring creep on a rotor groove). Given this disclosure, Appellant has failed to explain adequately why one skilled in the art would not have been capable of applying Telfer' s creep monitoring technique for turbine components to specific turbine components, such as a rotor groove, and reasonably expect this technique to provide the requisite creep monitoring to determine the timing for replacing a rotor groove. In re O'Farrell, 853 F.2d 894, 904 (Fed. Cir. 1988) ("For obviousness under§ 103, all that is required is a reasonable expectation of success."). Appellant's arguments are misplaced because the Examiner is only relying on Pross for its teaching that a turbine rotor is known to undergo creep during use that needs to be monitored. Final Act. 3; Ans. 4. Thus, Appellant's arguments do not point to Examiner error. Accordingly, we affirm the Examiner's prior art rejections of claims 1, 3-9, 12-16, and 18-23 under 35 U.S.C. § 103 (a) (Rejections I and II) for the reasons presented by the Examiner and given above. DECISION The Examiner's prior art rejections of claims 1, 3-9, 12-16, and 18- 23 under 35 U.S.C. § 103(a) are affirmed. TIME PERIOD No time period for taking any subsequent action in connection with this appeal may be extended under 37 C.F.R. § 1.136(a)(l )(iv). AFFIRMED 5 Copy with citationCopy as parenthetical citation